Optimal Blade Sequence Obtained from a Genetic Algorithm to Reduce the Mistuning Effects in a Bladed Disk Assembly
Author:
Funder
Korea University of Technology and Education
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1007/s12541-023-00940-2.pdf
Reference17 articles.
1. Lin, C.-C., & Mignolet, M. P. (1997). An adaptive perturbation scheme for the analysis of mistuned bladed disks. ASME Journal of Engineering for Gas Turbines and Power, 119, 153–160.
2. Whitehead, D. S. (1998). The maximum factor by which forced vibration of blades can increase due to mistuning. ASME Journal of Engineering for Gas Turbines and Power, 120, 115–119.
3. Castanier, M. P., & Pierre, C. (2006). Modeling and analysis of mistuned bladed disk vibration: Status and emerging directions. Journal of Propulsion and Power, 22(2), 384–396.
4. Lim, S.-H., Bladh, R., Castanier, M. P., & Pierre, C. (2007). Compact, generalized component mode mistuning representation for modeling bladed disk vibration. AIAA Journal, 45(9), 2285–2298.
5. Cha, D. (2020). Response of large mistuned bladed disk assembly subjected to random excitations. Journal of Mechanical Science and Technology, 34(2), 603–615.
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